View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 48271U 26145.60764016 +.00000000 +00000-0 +29469-3 0 00006
2 48271 97.5737 204.9199 0007203 59.4584 300.7353 15.05914613 09
| Epoch (UTC): | 25 May 2026 14:35:00 |
| Eccentricity: | 0.0007203 |
| inclination: | 97.5737° |
| perigee height: | 544 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 204.9199° |
| argument of perigee: | 59.4584° |
| revolutions per day: | 15.05914613 |
| mean anomaly at epoch: | 300.7353° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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